As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STATION 31J - INSPECTION FOUND A .75 INCH CRACK ON LOWER END OF THE THIRD VERTICAL STIFFENER OF RIGHT WING LEADING EDGE INBOARD RIB AT WS 75. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2. (M)